What is it about?
The problem of intercepting a moving target at a desired time with a desired impact time is solved by means of shaping the angle between the missile velocity vector and the line of sight as a general polynomial. The order of the polynomial determines the curvature of the trajectory. The simulation results confirm the utility of the proposed guidance law.
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This page is a summary of: Impact Time and Angle Control Against Moving Targets with Look Angle Shaping, Journal of Guidance Control and Dynamics, May 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004762.
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